View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 54060U 26145.22423075 +.00000000 +00000-0 +22546-4 0 00004
2 54060 53.2126 330.2007 0001737 98.2577 261.8612 15.08836047 05
| Epoch (UTC): | 25 May 2026 05:22:53 |
| Eccentricity: | 0.0001737 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 330.2007° |
| argument of perigee: | 98.2577° |
| revolutions per day: | 15.08836047 |
| mean anomaly at epoch: | 261.8612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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